2D and 3D thermoelastic phenomena in double wall transpiration cooling systems for gas turbine blades and hypersonic flight-Reference-Cited by-同舟云学术

2D and 3D thermoelastic phenomena in double wall transpiration cooling systems for gas turbine blades and hypersonic flight

Published:2021-06 Issue: Volume:113 Page:106610
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Skamniotis Christos,Cocks Alan C.F.^ORCID

Funder

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference55 articles.

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2. Advanced Gas Turbine Cooling: Double-Wall Turbine Cooling Technologies in Turbine NGV/Blade Applications;Murray,2019

3. Transpiration cooling using porous material for hypersonic applications;Cerminara,2019

4. An integrated conjugate computational approach for evaluating the aerothermal and thermomechanical performance of double-wall effusion cooled systems;Murray,2017

5. Effects of compound angle on film cooling effectiveness considering endwall lateral pressure gradient;Zhang;Aerosp. Sci. Technol.,2020

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